431 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Busek's highest power Hall effect thruster, 20 kW / 1 N thrust, throttleable 5-22 kW, tested at AEDC…
First US-built Hall effect thruster flown in space, flight heritage on TacSat-2, FalconSat-5/6, 13 mN thrust, 1390s Isp.
2kW-class Hall effect thruster with center-mounted cathode, 101 mN nominal thrust, 1710s Isp, xenon/krypton/iodine compatible.
Compact 100W Hall effect thruster with magnetic shielding for 10,000+ hour lifetime, 7 mN thrust, xenon/iodine compatible.
1N hydrogen peroxide monopropellant micro-thruster: 200s Isp, 30g, 2W, unique metal gauze catalyst, <100,000 pulses, for small satellite…
Long-life 1N hydrogen peroxide monopropellant micro-thruster: 120s Isp, 20g, 2W, innovative metal gauze catalyst, >500,000 demonstrated pulses.
Green monopropellant micro-thruster: 0.1N thrust, 110s Isp, 11g, 0.5W, hydrogen peroxide with metal gauze catalyst, <500,000 demonstrated pulses.
Compact hydrogen peroxide monopropellant micro-thruster: 0.5N thrust, 170s Isp, 15g, 1W, metal gauze catalyst, <100,000 pulses, for small…
Long-life hydrogen peroxide monopropellant micro-thruster: 0.5N thrust, 120s Isp, 15g, 1W, metal gauze catalyst, <500,000 demonstrated pulses.
Ultra-miniature Tridyne cold-gas micro-thruster: 0.005N thrust, 150s Isp, 10g, 0.5W, non-toxic propellant, <100,000 pulses, for CubeSat and nanosatellite…
Green monopropellant micro-thruster: 0.005N thrust, 100s Isp, 10g, 0.5W, hydrogen peroxide with metal gauze catalyst, <500,000 pulse life,…
Miniature cold-gas micro-thruster: 0.05N thrust, 160s Isp, 12g, 0.5W, Tridyne non-toxic propellant, <100,000 pulses, for CubeSat and nanosatellite…
IHI Aerospace flight-proven 478N bipropellant thruster using MMH/MON3 with 316s Isp, 15,000s demonstrated life, for apogee kick and…
Qualified 6kW xenon Hall-effect thruster delivering over 359mN thrust and up to 1783s specific impulse for all-electric satellites.
IHI Aerospace flight-proven 22N bipropellant thruster using Hydrazine/NTO with 295s Isp and 583 kg demonstrated propellant throughput.
IHI Aerospace flight-proven 124N bipropellant thruster using MMH/MON3 with 274.9s Isp, 40,000s demonstrated life and 446 kg throughput.
IHI Aerospace flight-proven 50N hydrazine monopropellant thruster with 225s Isp, >14,000 demonstrated pulses and >107 kg throughput.
IHI Aerospace flight-proven 450N bipropellant thruster using Hydrazine/NTO with 326s Isp and 32,850s demonstrated total impulse life.
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